GB746377A - Improvements in or relating to gas turbine installations - Google Patents

Improvements in or relating to gas turbine installations

Info

Publication number
GB746377A
GB746377A GB1187153A GB1187153A GB746377A GB 746377 A GB746377 A GB 746377A GB 1187153 A GB1187153 A GB 1187153A GB 1187153 A GB1187153 A GB 1187153A GB 746377 A GB746377 A GB 746377A
Authority
GB
United Kingdom
Prior art keywords
turbine
condenser
compressor
heat exchanger
exhaust
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB1187153A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB1187153A priority Critical patent/GB746377A/en
Publication of GB746377A publication Critical patent/GB746377A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K21/00—Steam engine plants not otherwise provided for
    • F01K21/04—Steam engine plants not otherwise provided for using mixtures of steam and gas; Plants generating or heating steam by bringing water or steam into direct contact with hot gas
    • F01K21/042—Steam engine plants not otherwise provided for using mixtures of steam and gas; Plants generating or heating steam by bringing water or steam into direct contact with hot gas pure steam being expanded in a motor somewhere in the plant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
    • F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
    • F01K23/06—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
    • F01K23/10—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle with exhaust fluid of one cycle heating the fluid in another cycle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

746,377. Turbine plant. BARKER, A. Dec. 4, 1953 [April 29, 1953], Nc. 11871/53- Class 110(3) A gas turbine plant in which heat is transferred in a heat exchanger from the exhaust gases to a condensible secondary working fluid which is injected into the combustion chamber or chambers has a condenser through which the gases and secondary fluid leaving the heat exchanger are passed and means for controlling the condenser temperature so as to determine the amount of secondary fluid which passes through the condenser to atrriosphere. A compressor 2 supplies air to a series of combustion chambers 5 feeding a turbine 8 driving the compressor. Fuel is supplied to the combustion chambers by an engine driven pump 7. The turbine exhaust gases enter a casing 9 containing a heat exchanger comprising coils of piping 11, 12 and baffle means 13, 14, 15, 16. The gases leaving the casing 9 pass into a direct contact condenser 18 provided with sprays 19, and exhaust to atmosphere through the duct 20. Condensate is collected in the well 21 and delivered by a pump 22 to the inlet 23 of the coils 11, 12. The steam raised in the heat exchanger is led to a steam turbine 25 mounted on the shaft 1 between the compressor 2 and gas turbine 8. The exhaust from the turbine 25 is mixed with the air supplied to the combustion chamber in the ducts 26. The turbine 25 may be dispensed with, if desired. The pump 22 also supplies water for direct injection into the compressor intake through a pipe 27 and through a pipe 28 to a cooler or radiator 29 from which the cooled water is supplied to the condenser sprays through pipes 30, 31. The branch pipe 28 is controlled by a valve 32 actuated by a float 33 in the condenser well. A compressor 34 may be provided to supply cooling air to the rear bearing 35. A secondary fluid other than water may be used.
GB1187153A 1953-04-29 1953-04-29 Improvements in or relating to gas turbine installations Expired GB746377A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1187153A GB746377A (en) 1953-04-29 1953-04-29 Improvements in or relating to gas turbine installations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1187153A GB746377A (en) 1953-04-29 1953-04-29 Improvements in or relating to gas turbine installations

Publications (1)

Publication Number Publication Date
GB746377A true GB746377A (en) 1956-03-14

Family

ID=9994191

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1187153A Expired GB746377A (en) 1953-04-29 1953-04-29 Improvements in or relating to gas turbine installations

Country Status (1)

Country Link
GB (1) GB746377A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2920448A (en) * 1955-07-29 1960-01-12 Sebac Nouvelle Sa Apparatus for imparting rapid speed to a mass of fluid
US3396538A (en) * 1966-10-03 1968-08-13 United Aircraft Corp Water injection for thrust augmentation
US3739575A (en) * 1972-04-05 1973-06-19 D Falk Combustion gas recirculating turbine engine
WO1980000864A1 (en) * 1978-10-26 1980-05-01 I Rice Reheat gas turbine
EP0319699A2 (en) * 1987-11-30 1989-06-14 General Electric Company Steam injected engine with auxillary high pressure steam turbine
GB2228295A (en) * 1988-12-14 1990-08-22 Gen Electric Cooling a turbine engine
US8250854B2 (en) 2007-12-05 2012-08-28 Sharpe Thomas H Self-starting turbineless jet engine
EP4442976A1 (en) * 2023-03-24 2024-10-09 MTU Aero Engines AG Turbomachine for an aircraft engine

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2920448A (en) * 1955-07-29 1960-01-12 Sebac Nouvelle Sa Apparatus for imparting rapid speed to a mass of fluid
US3396538A (en) * 1966-10-03 1968-08-13 United Aircraft Corp Water injection for thrust augmentation
US3739575A (en) * 1972-04-05 1973-06-19 D Falk Combustion gas recirculating turbine engine
WO1980000864A1 (en) * 1978-10-26 1980-05-01 I Rice Reheat gas turbine
EP0020594A1 (en) * 1978-10-26 1981-01-07 Ivan G Rice Reheat gas turbine.
EP0020594A4 (en) * 1978-10-26 1981-02-12 Ivan G Rice Reheat gas turbine.
EP0319699A2 (en) * 1987-11-30 1989-06-14 General Electric Company Steam injected engine with auxillary high pressure steam turbine
EP0319699A3 (en) * 1987-11-30 1989-09-20 General Electric Company Steam injected engine with auxillary high pressure steam turbine
GB2228295A (en) * 1988-12-14 1990-08-22 Gen Electric Cooling a turbine engine
US4982564A (en) * 1988-12-14 1991-01-08 General Electric Company Turbine engine with air and steam cooling
GB2228295B (en) * 1988-12-14 1992-12-16 Gen Electric Cooling a turbine engine
US8250854B2 (en) 2007-12-05 2012-08-28 Sharpe Thomas H Self-starting turbineless jet engine
EP4442976A1 (en) * 2023-03-24 2024-10-09 MTU Aero Engines AG Turbomachine for an aircraft engine

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